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EASA PART-66 MODULE 14
14.1 Turbine Engines
(a) Constructional arrangement and operation of turbojet, turbofan, turboshaft and turbopropeller engines;
(b) Electronic Engine control and fuel metering systems (FADEC).
14.2 Engine Indicating Systems
Exhaust gas temperature/Interstage turbine temperature systems;
Engine Thrust Indication: Engine Pressure Ratio, engine turbine discharge pressure or jet pipe pressure systems;
Oil pressure and temperature;
Fuel pressure, temperature and flow;
These EASA module pages provide subject lists to guide you through the regulations. Exams can be taken at A, B1 or B2 level, it is best to take at the higher level to prevent having to re-take later.
Note1: Higher (more difficult) level in brackets after module name. Where 'Either' shown indicates similar levels.
Note 2: If Module 15 passed at B1 Module 14 not required for B2. Otherwise Module 14 required for B2 only.
Note 3: Module 4 not required for Category A level.
MODULE 14 BOOK
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